View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56005U 26145.26669171 +.00000000 +00000-0 +52771-4 0 00001
2 56005 43.0007 351.1692 0001029 280.0573 80.0162 15.27577804 09
| Epoch (UTC): | 25 May 2026 06:24:02 |
| Eccentricity: | 0.0001029 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 351.1692° |
| argument of perigee: | 280.0573° |
| revolutions per day: | 15.27577804 |
| mean anomaly at epoch: | 80.0162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|